JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5300' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5300' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AWXA0002255Support · corrodedD: Corrosion on floor support Hat section at station 405 between RBL 25 to RBL 45.C: Removed and fabricated and installed floor support Hat section at STA 405 between RBL 25 to 45 IAW SRM 51-10-2 pg 12, 51-40-02 pg 1 SRM 51-20-01 pg 1SDR HNAA0100062Strap · corrodedSKIN JOINT STRAP BETWEEN STRINGERS 20S AND 22S AT STATION X370.80 IS CORRODED. REPAIRED STRAP IAW EO8-53-01-399.SDR AALA20011719Stringer · corrodedTUL - FOUND STRINGER 24L DENTED AT STATION 460. CUT AND REMOVED DAMAGED SECTION OF STRINGER. SPLICED IN NEW SECTION OF STRINGER PER SRM 53-10-3. (M)SDR USAA011142Bulkhead · gougedCLT - FOUND PRESSURE AFT BULKHEAD WITH 3 GOUGES APPROXIMATELY .125 INCH, LBL 3 BS 1016. INSTALLED DOUBLER, TRIPLER, FILLER OF REPAIR PER EA 85254. (M)SDR USAA011125SkinCLT - FOUND SKIN WITH LIGHTNING STRIKE, BS 620 - 2.5 INCH, BETWEEN STRINGER 18L AND 19L. DRILLED OUT DAMAGE AND INSTALLED RIVET PER SRM 53-00-01. (M)SDR WXOA01012BStringer · crackedLAS - AIRCRAFT FUSELAGE DAMAGED BY GROUND SERVICE EQUIPMENT WITH AIRCRAFT POSITIONED AT GATE. DAMAGE IDENTIFIED AS PUNCTURED FUSELAGE SKIN AT FUSELAGE STATION 1022 LEFT BETWEEN LONGERON 24L AND 26L, AND CRACKED STRINGER AT FUSELAGE STATION 1022L LONGERON 26L.SDR USAA011138Skin · crackedCLT - FOUND SKIN CRACKED 4 INCHES, BS 787 BS 25L. INSTALLED DOUBLER AND FILLER PER SRM 53-00-01 FIG 217. (M)SDR USAA011107Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, BS 727 D AND 3 INCHES AT STRINGER 23L. INSTALLED DOUBLER PER TR 53-60-03. (M)SDR USAA011108Skin · crackedCLT - FOUND SKIN CRACKED 2 INCHES, BS 727D PLUS 17 INCHES STRINGER 24R. INSTALLED DOUBLER PER SRM 53-00-01. (M)SDR USAA011111Web · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 297 BS 9R CUTOUT STRUCTURE. INSTALLED REPAIR AND REPAIR PARTS PER SRM 51-40-02. (M)SDR USAA011112Stiffener · crackedCLT - FOUND STIFFENER CRACKED .5 INCH, BS 900 STRINGER 11L. INSTALLED NEW PART PER SRM 51-10-2. (M)SDR USAA011113Frame · dentedCLT - FOUND FRAME DENTED .5 INCH BY .5 INCH BY .035 INCH, BS 827 STRINGER 24-251. INSTALLED FRAME DOUBLER PER TR 53-60-07. (M)SDR USAA011103Tie ClipCLT - FOUND TIE CLIP WITH WRONG TYPE CLIP INSTALLED, BS 596-S9L. INSTALLED NEW TIE CLIP PER EO NR 5393G227. (M)SDR USAA011100Web · corrodedCLT - FOUND FLOORBEAM WEB CORRODED, BS 344 FLOORBEAM, LBL 14.5 TO 21.5. CORROSION LEVEL 1, TASK NR C53-107-01. BLENDED OUT CORROSION, INSTALLED DOUBLER AND TRIPLER PER EA 85198. (M)SDR COMA0160619Angle · corrodedTHE FWD "J" ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL9 IS CORRODED.REMOVED AND REPLACED FWD "J" ANGLE USING NEW PART NUMBER 600-34017-351 ANGLE I/A/W WVAC EO 601R-53-2649.SDR COMA0160618Angle · corrodedAFT "J" ANGLE AT F.S. 280.00 CORRODED.REMOVED AND REPLACED AFT "J" ANGLE AT F.S. 280.00 BY FABRICATING NEW ANGLE AND INSTALLING I/A/W WVAC EO 601R-53-2650.SDR COMA0160617Plate · improperTWO SPLICE PLATES WERE FABED INCORRECTLY BY MANUFACTURER.FABRICATED TWO DOUBLER PLATES, REWORKED SPLICE PLATES, INSTALLED DOUBLER PLATES AND INSTALLED REWORKED SPLICE PLATES I/A/W WVAC E.O. 601R-53-2654.SDR 2001UALA01750Crease Beam · corrodedCABIN FLOOR INNER CREASE BEAM BELOW DOR 2L DRAIN GUTTER HAS EXCESSIVE CORROSION STA.700 TO 720 LBL70" STRINGER 17L. MAJOR REPAIR ACCOMPLISHED. REMOVED SECTION OF INNER CREASE BEAM L-ANGLE Z ANGLE IN DOORWAY FROM STA.665 TO 754 AT FACTORY SPLICES INSTALLED NEWSDR USAA011178Skin · crackedTPA - FOUND SKIN CRACKED 1 INCH, STATION 947.5 UPPER FORWARD CORNER HINGE CUT OUT. INSTALLED DOUBLERS PER SRM 53-60-01 FIG 205. (M)SDR ABXA010467Fitting · corrodedLEFT SLANT PANEL, OUTBOARD ATTACH FITTING WAS CORRODED. REPLACED FITTING IAW DC-9 SRM 51-30-5.SDR COMA0160602Angle · corrodedPASSENGER DOOR LOWER THRESHOLD CORRODED.REMOVED AND REPLACED THRESHOLD SUPPORT ANGLE I/A/W WVAC EO 601R-53-2643.SDR COMA0160601Angle · corrodedFORWARD J ANGLE AT FS 280 BETWEEN LBL9 AND RBL 9 IS CORRODED.REMOVED AND REPLACED FORWARD J ANGLE I/A/W WVAC EO 601R-53-2640.SDR USAA011096SkinCLT - FOUND SKIN OIL CAN IN AFT PRESSURE BULKHEAD, BS 1016. INSTALLED DOUBLER PER SRM 53-80-08 FIG 201. (M)SDR USAA011176Stringer · corrodedTPA - FOUND STRINGER CORRODED 6 SQUARE INCH AREA, STRINGER 25L STATION 967 PLUS 10 INCHES. CORROSION LEVEL 2. SPLICED IN SECTION OF STRINGER PER SRM 53-00-03 PAGE 201-204. (M)SDR USAA011090RivetCLT - FOUND WORKING RIVET, BS 889 AND 12R. INSTALLED NEW RIVET PER SRM 51-40-00. (M)SDR SIMA200123405Beam · corrodedSBP - DURING MBV INSPECTION, MAINTENANCE FOUND THE LEFT GALLEY FLOOR FRAME AND INBOARD BRACKET CORRODED. REMOVED AND REPLACED INTERCOSTAL AND L ANGLE IAW SAAB SRM 51-40-21. (M)SDR SIMA200123404Track · corrodedSBP - DURING MBV INSPECTION, MAINTENANCE FOUND THE RIGHT GALLEY TRACK IS CORRODED. REMOVED AND REPLACED GALLEY TRACK AND PROFILE IAW SAAB SRM 51-40-40, 51-40-21, AND 51-40-22. (M)SDR USAA011089Skin · dentedCLT - FOUND SKIN DENTED AND GOUGED 1 INCH BY .070 INCH, BS 309 JUST BELOW BS 24R. FABRICATED AND INSTALLED FILLERS AND REPAIR DOUBLERS PER SRM 53-30-3 FIG 42. (M)SDR USAA011086Angle · crackedCLT - FOUND ANGLE CRACKED .5 INCH, BS 328 FLOORBEAM RBL 31.5 TO INTERCOSTAL. FABRICATED REPAIR DOUBLER PER SRM 53-10-02. (M)SDR USAA011085Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, BS 359 S11L. REMOVED AND REPLACED PART WITH PART NR 1126212 PER 51-10-1. (M)SDR USAA011093Web · corrodedCLT - FOUND CREASE BEAM WEB CORRODED 10 SQUARE INCHES, LEFT SIDE BS 927-947. FABRICATED NEW WEB PER DRAWING 65-52878 AND INSTALLED PER SRM 51-30-2. (M)SDR ABXA010466Panel · corrodedLEFT SLANT PANEL WAS CORRODED AROUND THE LOWER NUTPLATES. LEVEL II CORROSION. INSTALLED NEW SLANT PANEL IAW DC-9 SRM 51-30-1.SDR ABXA010465Panel · corrodedRIGHT SLANT PANEL WAS CORRODED AROUND NUTPLATES ON THE LOWER EDGE OF PANEL. LEVEL II CORROSION. INSTALLED NEW SLANT PANEL IAW DC-9 SRM.SDR AALA20011642FrameTUL - FOUND DENT IN TOP FLANGE OF FRAME STATION 313 BETWEEN LONGERON 24L-25L. REPAIRED FRAME PER AARD 53-10-00-17. (M)SDR USAA011062Stringer · dentedCLT - FOUND STRINGER DENTED .5 INCH, STRINGER 16L STATION 400. FABRICATED REPAIR CHANNEL, STRINGER TIE CLIP PER EA 85178. (M)SDR USAA011063Strap · damagedCLT - FOUND FRAME AND STRAP HAS DRILL DAMAGE .25 INCH, AFT FLANGE OF FRAME AND STRAP, BS 493 ABOVE BS 25R. INSTALLED DOUBLER AT FRAME AND STRAP PER SRM 53-00-07, SRM 51-70-11. (M)SDR USAA01061Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .75 INCH, BS 300.5 TO BS 301.5 S10L. INSTALLED NEW ANGLE PER SRM 51-10-1. (M)SDR USAA011059Web · crackedCLT - FOUND WEB CRACKED TWO PLACES .060 INCH, BULKHEAD WEB AT ATTACH TO 1016 Y CHORD. INSTALLED DOUBLER PER SRM 53-10-4 AND SRM 51-30-5. (M)SDR USAA011058Frame · dentedCLT - FOUND FRAME DENTED .25 INCH, BS 827 AT S24L UPPER CHORD. INSTALLED FRAME DOUBLER PER SRM 53-10-4. (M)SDR USAA011057Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, BS 359 S14L. REMOVED AND REPLACED WITH PART NR 1131272 PER SRM 51-10-01. (M)SDR USAA011055Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH, BS 380 STRINGER 26L. FABRICATED REPLACEMENT PART PER SRM 53-10-04. (M)SDR GAIA01296STFrame · damagedDURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE BS 600 FRAME WAS DAMAGED AT STRINGER S17R. REPAIRED IAW BOEING 727 SRM 51-40-3, FIGURE 1 PAGE 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR USAA011071Beam · corrodedPIT - FOUND BEAM CORRODED, LBL 48 INCHES-RBL 48 INCHES, STATION 986.5 CABIN FLOOR LBL 48 INCHES RBL 48 INCHES. REPLACED UPPER CHORD PER TYPICAL REPAIR 53-10-05. (M)SDR USAA011072Beam · corrodedPIT - FOUND BEAM CORRODED LBL 60 INCHES - RBL 60 INCHES, STATION 328 CABIN FLOOR LBL 60 INCHES, RBL 60 INCHES. REMOVED CORROSION, TREATED AND PRIMED PER SRM 53-10-51. (M)SDR USAA011067Web · corrodedPIT - FOUND WEB CORRODED 4 INCHES BY 2 INCHES, STATION 867 RIGHT CREASE BEAM WEB. CORROSION LEVEL 1, TASK NR C53-107-01. BURNISHED, TREATED AND PRIMED AND PAINTED PER SRM 51-10-02. (M)SDR USAA011068Web · corrodedPIT - FOUND WEB CORRODED 8 INCH BY 4 INCH AREA OF CORROSION, STATION 887 LEFT CREASE BEAM WEB. CORROSION LEVEL 1, TASK NR C53-107-01. BURNISHED, TREATED, PRIMED AND PAINTED PER SRM 51-10-02. (M)SDR USAA011073Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, BOTTOM OF VERTICAL FRAME ATTACH AREA AT WING BOX. (M)SDR USAA011074Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, STATION 787 RIGHT BETWEEN STRINGER 8/9. (M)SDR USAA011075Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, STATION 787 LEFT BETWEEN STRINGER 8/9. (M)SDR USAA011076Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, STATION 867 RIGHT BETWEEN STRINGER 8/9. (M)
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